WO1996036485A1 - Composite supraconducteur a plusieurs filaments et procede de fabrication - Google Patents

Composite supraconducteur a plusieurs filaments et procede de fabrication Download PDF

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Publication number
WO1996036485A1
WO1996036485A1 PCT/US1996/007061 US9607061W WO9636485A1 WO 1996036485 A1 WO1996036485 A1 WO 1996036485A1 US 9607061 W US9607061 W US 9607061W WO 9636485 A1 WO9636485 A1 WO 9636485A1
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Prior art keywords
matrix
filament
oxide
filaments
decoupling layers
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PCT/US1996/007061
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English (en)
Inventor
Gregory L. Snitchler
Gilbert N. Riley, Jr.
Alexis P. Malozemoff
Craig J. Christopherson
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American Superconductor Corporation
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Priority to EP96914661A priority Critical patent/EP0828606A4/fr
Priority to AU57956/96A priority patent/AU709214B2/en
Priority to JP53505796A priority patent/JP3444893B2/ja
Priority to NZ308348A priority patent/NZ308348A/en
Publication of WO1996036485A1 publication Critical patent/WO1996036485A1/fr

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    • H—ELECTRICITY
    • H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
    • H10N—ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
    • H10N60/00—Superconducting devices
    • H10N60/01—Manufacture or treatment
    • H10N60/0268—Manufacture or treatment of devices comprising copper oxide
    • H10N60/0801—Manufacture or treatment of filaments or composite wires
    • H—ELECTRICITY
    • H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
    • H10N—ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
    • H10N60/00—Superconducting devices
    • H10N60/20—Permanent superconducting devices
    • H10N60/203—Permanent superconducting devices comprising high-Tc ceramic materials
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00—Stock material or miscellaneous articles
    • Y10S428/922—Static electricity metal bleed-off metallic stock
    • Y10S428/9265—Special properties
    • Y10S428/93—Electric superconducting
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S505/00—Superconductor technology: apparatus, material, process
    • Y10S505/70—High TC, above 30 k, superconducting device, article, or structured stock
    • Y10S505/704—Wire, fiber, or cable
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49002—Electrical device making
    • Y10T29/49014—Superconductor
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24942—Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/29—Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
    • Y10T428/2913—Rod, strand, filament or fiber
    • Y10T428/2933—Coated or with bond, impregnation or core
    • Y10T428/294—Coated or with bond, impregnation or core including metal or compound thereof [excluding glass, ceramic and asbestos]

Definitions

  • This invention relates to superconducting oxide articles having improved characteristics for alternating current operation and to a method for manufacturing them.
  • the invention relates to composite articles comprising multiple substantially electrically decoupled domains, each containing one or more fine filaments of a superconducting oxide material, and to methods and intermediates for manufacturing such composites.
  • Superconducting oxide materials alone do not possess the necessary mechanical properties, nor can they be produced efficiently in continuous long lengths.
  • Superconducting oxides have complex, brittle, ceramic-like structures which cannot by themselves be drawn into wires or similar forms using conventional metal-processing methods. Moreover, they are subject to a magnetic effect known as flux jumping which causes sudden localized temperature variations that can force them out of their superconducting state if it is not compensated. Consequently, the more useful forms of high temperature superconducting conductors usually are composite structures in which the superconducting oxides are supported by a matrix material which adds mechanical robustness to the composite and provides good thermal dissipation in the event of flux jumping.
  • the matrix material chosen must be readily formable, have high thermal conductivity, and be sufficiently non-reactive with respect to the superconducting oxides under the conditions of manufacturing and use that the properties of the latter are not degraded in its presence.
  • composites made by the popular powder-in-tube or PIT process described, for example, in US Patent Nos . 4, 826, 808, and 5, 189, 009 to Yurek et al . and N. Gao & J. Vander Sande, Superconducting Science and Technology, Vol . 5, pp. 318-326, 1992; C. H. Rosner, M.S. Walker, P. Haldar, and L . R.
  • the superconductor geometry must be selected to reduce AC losses, in order to preserve the intrinsic advantage of superconductors, the absence of DC electrical resistance.
  • the physics governing AC losses in low temperature superconducting composite materials have been described and analyzed, c.f. Wilson, Superconducting Magnets, Ch 8 (1983, 1990) , W.J. Carr, Jr. , AC loss and macroscopic theory of superconductors, Gordon and Breach Science Publishers, New York, 1983 , . and would be expected to operate in superconducting oxide composites with similar geometries.
  • the primary sources of AC loss are hysteretic loss within the superconducting filament(s) ,and eddy current loss in the matrix enhanced by coupling between superconducting filament(s) .
  • the superconductor is preferably subseparated into many small filaments that are discrete and dimensionally uniform along the length of the conductor. Eddy current losses may be minimized by increasing the electrical resistivity of the matrix or by twisting the filaments, with tighter twist pitches providing lower losses.
  • the inherent chemical and mechanical limitations of superconducting oxide composites limit the degree to which these approaches may be relied on for reducing AC losses in high temperature superconducting composites. Conventional methods for increasing the resistivity of the matrix have also been limited.
  • Silver the matrix material of choice for these composites for the reasons discussed above, has a very low electrical resistivity.
  • Efforts have been made to increase the resistivity of the matrix, for example, by distributing small amounts of oxide-forming metals in finely separated form in a silver matrix, and by using higher resistivity alloys to form all or part of the matrix adjacent to the filaments.
  • the presence of even very small amounts of chemically reactive materials near the filament/matrix boundary during the manufacturing process can significantly degrade the properties of the superconducting oxide composite. This is a particularly delicate issue for composites consisting of many fine filaments as the higher surface to volume ratio greatly increases the risk of contamination.
  • layers of high resistivity material can also block oxygen access to the filaments during manufacturing, inhibiting the formation of the superconducting oxide from its precursors.
  • increasing the electrical resistivity of the matrix adjacent to the filaments, whether by surrounding the filaments with a resistive layer or by providing a uniformly doped matrix generally decreases its thermal conductivity, increasing the risk of flux jumping during use.
  • an object of the invention is to provide multifilamentary superconducting composite articles in any desired aspect ratio with improved AC loss characteristics and high critical current densities, and a method for manufacturing them.
  • Another object of the invention is to provide a method of reducing coupling losses in multifilamentary superconducting oxide composite articles without significantly increasing the risk of contamination of the superconducting filaments by the supporting matrix.
  • Another object of this invention is to provide a method of manufacturing superconducting composite articles suitable for AC applications which provides adequate oxygen access for formation of a desired superconducting oxide with optimal current carrying capacity.
  • Another object of the invention is to provide highly aspected multifilamentary BSCCO 2212 and 2223 composite conductors having high current densities, superior AC loss characteristics and robust mechanical properties, and a method for producing them.
  • the invention provides a multifilamentary superconducting composite article comprising multiple substantially electrically decoupled domains, each including one or more fine, preferably twisted filaments comprising a desired superconducting oxide material. Tapes, wires and other elongated multifilamentary articles are preferred forms of the article.
  • the article comprises a matrix, at least one discrete filament decoupling layer comprising an insulating material, which is disposed within the matrix to separate the matrix into a plurality of substantially electrically decoupled domains; a plurality of filaments, each comprising a desired superconducting oxide, which are disposed within or around and preferably essentially encapsulated by the matrix and chemically isolated thereby from the decoupling layers, each of the substantially electrically decoupled domains containing at least one filament.
  • the invention provides reductions in coupling losses roughly proportional to the square of the article's cross- sectional ratio. It facilitates the production of multifilamentary articles that exhibit good DC performance characteristics and markedly superior AC performance, particularly in highly aspected forms.
  • the invention provides an intermediate for a multifilamentary superconducting composite article comprising multiple domains, each including one or more fine, preferably twisted filaments of a superconducting oxide material.
  • the intermediate comprises a matrix, at least one discrete filament decoupling layer comprising an insulating material or its predecessor, which is disposed within the matrix to separate the matrix into a plurality of substantially separate domains; a plurality of fine, preferably twisted filaments, each comprising a desired superconducting oxide or its precursors, which are disposed within or around and preferably essentially encapsulated by the matrix and chemically isolated thereby from the decoupling layers, each of the separate domains containing at least one filament.
  • filament decoupling layers are meant discrete layers comprising insulating materials or their predecessors, in geometric forms of sufficient dimension to significantly increase the resistance between domains in the finished article.
  • each domain is at least partially bounded by the surfaces of one or more filament decoupling layers but the arrangement and materials of the layers are selected so they do not substantially inhibit oxygen access to the filaments in the domain during processing.
  • the filament decoupling layers extend parallel to the filaments along the length of the article, and are very thin in proportion to their width and length. In cross section, they may resemble, for example, fins, donuts, stars, centipedes and combinations of these.
  • the thickness of the insulating material is less than the filament thickness, and preferably less than about 5 microns.
  • substantially electrically decoupled domain is meant that the direct high conductivity path between adjacent domains is at least 50% and preferably 85% occluded by the filament decoupling layers, but not more than 100%, preferably not more than 99% and most preferably not more than 95% occluded.
  • insulating material is meant a material with an electrical resistivity high in comparison to that of the matrix material used in the composite under the intended conditions of use. Typically, the insulating material selected will have resistivity at least 10 times higher than that of the selected matrix material. Materials with resistivities greater than about 20 m-ohm cm may be used, and materials with resistivities greater than about 100 m-ohm cm are most preferred. Elemental oxides, sulfides, nitrides, semiconductors, intermetallics and other non-metallic insulating materials are suitable.
  • predecessor as that term is used herein, is meant any material that can be converted to an insulating material by heat treatment under suitable conditions.
  • Metals with high oxidation rates particularly the transition metals, the alkaline earths, thallium, zirconium, niobium, molybdenum, aluminum and their alloys are preferred predecessor materials, and zirconium, niobium, molybdenum, hafnium, tantalum, tungsten, titanium, vanadium, manganese, cobalt, iridium, vanadium nickel,iron and chromium are particularly preferred. Zirconium, niobium, nickel,iron and molybdenum are most preferred.
  • matrix as that term is used herein, is meant a material or homogeneous mixture of materials which supports or binds a substance, specifically including the filaments, disposed within or around the matrix.
  • non-reactive metal as that term is used herein, is meant a metal which is substantially non-reactive with respect to oxide superconductors and precursors and to oxygen under the expected conditions (temperature, pressure, atmosphere) of manufacture and use.
  • Alloy is used herein to mean an intimate mixture of substantially metallic phases or a solid solution of two or more elements. Silver and other noble metals are the preferred matrix materials, but alloys substantially comprising noble metals, including ODS silver, may be used.
  • a conductive jacketing layer surrounds .the article.
  • Noble metals and alloys comprising noble metals, including ODS silver, are the most preferred jacketing layer materials, but other conductive materials, including composites of several different metals, may be used.
  • Jacketing layers made from a material with a resistivity at least equal to that of the matrix material may be used, and jacketing layers with a resistivity on the order of about 0.5 - 10 mohm are especially preferred.
  • oxide superconductor is meant the oxide superconductor intended for eventual use in the finished article.
  • the desired oxide superconductor is selected for its superior electrical properties, such as high critical temperature or critical current density.
  • precursor is meant any material that can be converted to a desired oxide superconductor upon application of a suitable heat treatment.
  • fine filaments are meant filaments with a cross-sectional dimension less than 750, and preferably less than 150 microns.
  • the invention provides a method of manufacturing a multifilamentary superconducting composite article having improved AC loss properties by first, forming a composite intermediate comprising multiple domains, each including one or more fine, preferably twisted filaments of a superconducting oxide material or its precursor, and then thermomechanically processing the intermediate at conditions sufficient to produce at least one of the effects of texturing, crack healing and, if a precursor to the desired superconducting oxide remains, phase transformation in the filament material under conditions which support the electrical separation of the domains.
  • the forming step includes the step of providing filament decoupling layers comprising insulating materials or their predecessors to provide the desired domain separation, and in the most preferred embodiment, the insulating material is formed in situ from its predecessor during the thermomechanical processing step.
  • the forming step includes the steps of forming composite comprising a matrix, which substantially comprises a noble metal, a plurality of discrete filament decoupling layers disposed within the matrix to separate the matrix into a plurality of substantially separate domains, each layer comprising an insulating material or its predecessor, and a plurality of filaments, each comprising a desired superconducting oxide or its precursors, which are disposed within or around and preferably essentially encapsulated by the matrix and chemically isolated thereby from the decoupling layers, each of the domains containing at least one filament; and next, deforming the intermediate to produce at least one of the effects of twisting the filaments and texturing the material comprised therein.
  • the forming step includes the steps of forming filament decoupling layers from an oxide-forming predecessor to an oxide insulating material and the thermomechanical processing step comprises the steps of, first, heat treating the composite at conditions sufficient to passivate the predecessor and form an insulating material from at least part of the predecessor material but not to induce substantial phase transformation in the filament material; and, thereafter thermomechanically processing the composite at conditions sufficient to produce at least one of the effects of texturing, crack healing and, if a precursor to the desired superconducting oxide remains, phase transformation in the filament material.
  • the process also includes the step of providing a conductive jacketing layer surrounding the article.
  • Figure 1 is a photograph of the cross-section of a composite article made in accordance with one aspect of the invention.
  • Figure 2 is a process flow diagram illustrating the manufacture of the composite article of Figure 1 in accordance with one aspect of the present invention.
  • Figure 3 is a schematic diagram of the cross- section of a composite article made in accordance with another preferred embodiment of the invention.
  • Figure 4 is a processing profile of a heat treatment sequence in accordance with one aspect of the invention.
  • FIG. 5 is a processing profile of a heat treatment sequence in accordance with another aspect of the invention.
  • Figure 6 is a processing profile of a heat treatment sequence in accordance with yet another aspect of the invention.
  • Figure 7 is a schematic diagram of the cross- section of a composite article made in accordance with another preferred embodiment of the invention.
  • Figure 8 is a schematic diagram of the cross- section of a composite intermediate made in accordance with another preferred embodiment of the invention.
  • Figure 9 is a schematic diagram of the cross- section of a composite article made from the intermediate of Figure 8.
  • the invention provides a multifilamentary superconducting composite article comprising multiple substantially electrically decoupled domains, each including one or more fine, preferably twisted filaments comprising a desired superconducting oxide material.
  • substantially electrically decoupled domain as that term is used herein, is meant that the direct high conductivity path between adjacent domains is at least 50% and preferably 85% occluded, but not more than 100%, preferably not more than 99% and most preferably not more than 95% occluded. Electrical separation of the domains is preferably provided by filament decoupling layers.
  • filament decoupling layers are meant discrete layers comprising insulating materials or their predecessors, in geometric forms of sufficient dimension to significantly increase the resistance between domains in the finished article.
  • each domain is at least partially bounded by the surfaces of one or more filament decoupling layers but the arrangement and materials of the layers are selected so they do not substantially inhibit oxygen access to the filaments in the domain during processing.
  • the filament decoupling layers extend parallel to the filaments along the length of the article, although they may be discontinuous or broken at intervals, and are very thin in proportion to their width and length.
  • the layers may be connected to one another along their length to partially or fully surround one or more filaments.
  • the filament decoupling layers may also be twisted. If the filament decoupling layers are discontinuous, a period of discontinuity greater than the period of the twist is preferred. In lateral cross-section, they may resemble, for example, fins, donuts, stars, centipedes and combinations of these. Configurations such as the star- in-star illustrated in FIG 3, the bag-of-donuts illustrated in FIG 7, and the centipede illustrated in FIG 8 are particularly preferred. Any number of filament decoupling layers, and any number of filaments may be used in any of these configurations. Preferred configurations contain large numbers of filament decoupling layers and small numbers of filaments in each domain, with one filament per domain being the most preferred configuration.
  • the filaments and filament decoupling layers will both be supported by a matrix material. Most typically, both will be embedded in and chemically isolated by the matrix material, although other arrangements, such as alternating strata of matrix material, filament decoupling layers and filaments are also within the scope of the invention.
  • the filament decoupling layers must comprise material which is insulating and also inert to the superconducting oxide and to the matrix under conditions of normal use, such as a metal oxide.
  • the material for the filament decoupling layer in either its final or a predecessor form, must be able to survive the physical deformations and high temperatures of typical superconducting composite manufacturing processes, such as the PIT process, without impairing the properties of the composite.
  • the deformation processing stage it must be flexible, and preferably malleable.
  • it must not migrate in sufficient quantity to poison the superconducting material.
  • insulating materials with a broad range of electrical properties may be used.
  • the insulating material selected should have an electrical resistivity greater than 20 ohm cm. Materials with resistivities at least 100 times higher than that of the matrix material used in the composite under the intended conditions of use, i.e. at cryogenic temperatures, are preferred.
  • the thickness of the insulating material should be less than the filament thickness, and preferably between about 0.01 - 5 microns, with the range between about 0.1 - 1 microns being most preferred.
  • the filament decoupling layers are formed in situ by oxidation of a metal layers during the composite manufacturing process.
  • transition metals the alkaline earths, thallium, zirconium, niobium, molybdenum, aluminum and their alloys are preferred predecessor materials, and zirconium, niobium, molybdenum, hafnium, tantalum, tungsten, titanium, vanadium, manganese, cobalt, iridium, vanadium nickel,iron and chromium are particularly preferred. Zirconium, niobium, nickel,iron and molybdenum are most preferred.
  • FIG. 1 A preferred embodiment of the invention is illustrated in Fig 1.
  • the figure shows a composite article 100 comprising a conductive jacketing layer 102 surrounding a matrix, 104, which substantially comprises a noble metal.
  • a plurality of discrete filament decoupling layers 118, 120, 122, 124, 126, 128, 136 are embedded in the matrix in an arrangement that separates the matrix into a plurality of, and preferably at least three, separate domains 106, 108, 110, 112, 114, 116.
  • Each decoupling layer is comprised of an insulating material.
  • the decoupling layers separate the matrix into a plurality of substantially electrically decoupled domains.
  • a plurality of filaments, 130, 132, 134, each comprising a desired superconducting oxide or its precursors, are also embedded within the matrix 104, so arranged that each domain includes at least one filament, but each filament is essentially encapsulated by the matrix.
  • the matrix chemically isolates each filament from the decoupling layers and from any neighboring filaments.
  • the invention may be practiced with any desired oxide superconductor or its precursors.
  • desired oxide superconductor is meant the oxide superconductor intended for eventual use in the finished article.
  • the desired oxide superconductor is selected for its superior electrical properties, such as high critical temperature or critical current density.
  • precursor is meant any material that can be converted to an oxide superconductor upon application of a suitable heat treatment. Precursors may include any combination of elements, metal salts, oxides, suboxides, oxide superconductors which are intermediate to the desired oxide superconductor, or other compounds which, when reacted in the presence of oxygen in the stability field of a desired oxide superconductor, produces that superconductor.
  • elements, salts, or oxides of copper, yttrium or other rare earths, and barium for the rare earth family of oxide superconductors there may be included elements, salts, or oxides of copper, yttrium or other rare earths, and barium for the rare earth family of oxide superconductors; elements or oxides of copper, bismuth, strontium, and calcium, and optionally lead, for the BSCCO family of oxide superconductors; elements, salts, or oxides of copper, thallium, calcium and barium or strontium, and optionally, bismuth and lead, for the thallium (TBSCCO) family of oxide superconductors; elements, salts, or oxides of copper, mercury, calcium, barium or strontium, and optionally, bismuth and lead, for the mercury (HBSCCO) family of oxide superconductors.
  • BSCCO family of oxide superconductors
  • oxide superconductor intermediate to the desired oxide superconductor is meant any oxide superconductor which is capable of being converted to the desired oxide superconductor.
  • the formation of an intermediate may be desired in order to take advantage of desirable processing properties, for example, a micaceous structure, which may not be equally possessed by the desired superconducting oxide.
  • Precursors are included " in amounts sufficient to form an oxide superconductor.
  • the precursor powders may be provided in substantially stoichiometric proportion. In others, there may be a stoichiometric excess or deficiency of any precursor to accommodate the processing conditions used to form the desired superconducting composite.
  • excess or deficiency of a particular precursor is defined by comparison to the ideal cation stoichio etry of the desired oxide superconductor.
  • doping materials including but not limited to the optional materials identified above, variations in proportions and such other variations in the precursors of the desired superconducting oxides as are well known in the art, are also within the scope and spirit of the invention.
  • the three-layer, high-Tc phase of a member of the BSCCO family of superconductors (BSCCO 2223) , such as Bi 2 Sr 2 Ca 2 Cu 3 ⁇ ⁇ or (Bi, Pb) 2 Sr 2 Ca 2 CU 3 ⁇ ⁇ , is one of the desired superconducting oxide most preferred for the operation of the present invention.
  • Composites including BSCCO 2223 have demonstrated the potential for superior mechanical and electrical performance at long lengths when adequately textured.
  • the current-carrying capacity of a superconducting oxide composite depends significantly on the degree of crystallographic alignment and intergrain bonding of the oxide grains, together known as "texturing", induced during the composite manufacturing operation.
  • BSCCO 2212 and BSCCO 2223 are described in Tenbrink, Wilhelm, Heine and Krauth, Development of Technical High-Tc Superconductor Wires and Tapes, Paper MF-1, Applied Superconductivity Conference, Chicago (March 23-28, 1992) , and Motowidlo, Galinski, Hoehn, Jr. and Haldar, Mechanical and Electrical Properties of BSCCO Multi filament Tape Conductors, paper presented at Materials research Society Meeting, April 12-15, 1993.
  • filaments of equal dimension will also be non-uniformly flattened by the texturing process, with significantly greater flattening and DIT texturing of filaments at the center of the tape than of filaments at the periphery of the tape and non-uniform distances between filaments causing undesirable asymmetries in current carrying capability and additional AC loss effects.
  • the inventors have found that the division of the matrix into a plurality of substantially electrically decoupled domains substantially improve the AC loss characteristics of the superconducting composite article.
  • the effect is particularly pronounced for highly aspected superconducting oxide composites, which have large eddy current coupling losses when exposed to changing magnetic fields normal to their wide faces.
  • the inventors believe that, by analogy to Carr's anisotropic continuum model for losses in a multistrand Rutherford cable, W.J. Carr, Jr. and V.T. Kovachev, "Interstrand eddy current losses in SSC magnets, " Cryogenics, submitted 1994. , the losses in the filament/matrix region of an aspected superconducting composite composed of multiple domains can be approximated by a term representing the normal conductance between adjacent filaments within a domain
  • the conductive jacket will have standard eddy current losses, which can be approximated by
  • the layer separating adjacent domains is an insulator whose resistivity far exceeds the resistivity within the domain, P perp will be very low in comparison to P n or P j and may be ignored. If one surface of the domain is bounded by a portion of the jacketing layer, then in the simplest case where only one filament is found in each domain, the normal coupling P n will take place through the jacketing layer rather than through the filament decoupling layers, and may be represented by
  • the invention provides a method of manufacturing a multifilamentary superconducting composite article having improved AC loss properties by first, forming a composite intermediate comprising multiple domains, each including one or more fine, preferably twisted filaments of a superconducting oxide material or its precursor, and then thermomechanically processing the intermediate at conditions sufficient to produce at least one of the effects of texturing, crack healing and, if a precursor to the desired superconducting oxide remains, phase transformation in the filament material under conditions which support the electrical separation of the domains.
  • the forming step includes the step of providing filament decoupling layers comprising insulating materials or their predecessors to provide the desired domain separation.
  • the invention may be used to manufacture these composite articles by processes such tape casting, dip coating, and a variety of sputtering and vapor deposition processes, it is particularly well-adapted for manufacturing processes, such as powder-in-wire or the well-known powder in tube (PIT) process, in which the filament material is converted from precursor to desired superconducting oxide while in intimate contact with an enclosing matrix.
  • PIT powder in tube
  • the matrix material selected must be readily formable and must be sufficiently non-reactive with respect to the superconducting material that the latter's properties are not substantially degraded in its presence. Moreover, it must allow good oxygen access to the filaments under the expected manufacturing conditions to facilitate formation of the desired superconducting oxides from their precursors.
  • Metals which are noble in that they are substantially non-reactive with respect to oxide superconductors and their precursors and to oxygen under the expected conditions (temperature, pressure, atmosphere) of manufacture and use are preferred, although alloys substantially comprising these metals, including oxide dispersion strengthened (ODS) silver, may also be used.
  • Preferred noble metals include silver (Ag) , gold (Au) , platinum (Pt) and palladium (Pd) . Silver and its alloys, being lowest in cost of these materials, are most preferred for large-scale manufacturing.
  • Fig 2 shows a process flow diagram for manufacturing a composite article, such as that shown in Fig 1, using PIT techniques in accordance with one aspect of the present invention.
  • a monofilamentary rod is formed by packing a precursor oxide powder into a metal container, such as a silver tube.
  • the metal containers are deformation processed to form monofilamentary rods of reduced diameter.
  • a bundling step a number of the rods are assembled in some close packed or other symmetric arrangement to form a multifilamentary composite. Filament decoupling layers are inserted among the rods in a predetermined geometry during the bundling step.
  • the layers may be in the form of sheets, foils, cores, or other shapes depending on the ultimate geometry desired. (For economies of scale, it is preferred that the decoupling layers be assembled into the composite at a relatively early stage of the manufacturing process, while the desired superconducting oxide is still in its more malleable precursor stage, but this is not required for the practice of the invention.)
  • filament decoupling layers of predecessor materials such as oxide forming materials selected from the group consisting of the transition metals, the alkaline earths, titanium, zirconium, niobium, molybdenum, aluminum, and their alloys, may be selected.
  • filament decoupling layers of insulating materials such as alumina or other metal oxides, nitrides, sulfides, semiconductors or intermetallics may be selected.
  • Step 206 is followed in step 208 by further deformation processing including longitudinal reductions and, for AC applications, preferably twisting, to form a multifilamentary intermediate having the desired number of filaments.
  • a preferred deformation sequence is drawing, then twisting, then rolling, but other deformation sequences may be used.
  • Steps 206 and 208 may be repeated as many times as desired, with the insertion of additional filament decoupling layers at each iteration, to provide an intermediate composite of reduced cross-section including the desired number of domains each defined by one or more filament decoupling layers and containing one or more twisted filaments of precursor material in intimate contact with a surrounding matrix, which substantially comprises a noble metal, . From one to five rebundling iterations are preferred.
  • a highly aspected superconducting tape 300 is shown, which may be manufactured by rebundling intermediates with one filament per domain, made in the general form of intermediate 100 shown in FIG l above with additional decoupling layers 304, 306, 308, and inserting the whole ensemble into a jacketing layer 302 for deformation and thermomechanical processing as described above.
  • the conductive jacketing layers shown in Figs 1 and 3 may be added to the intermediate during or after steps 206, 208, or 210.
  • the material for the jacketing layer must have an electrical resistivity at least equal to, and preferably 10 times that of the matrix material. Resistivities on the order of 0.5 -10 mohm cm are especially preferred.
  • the jacketing layer is chemically isolated from the filaments by the matrix, it may be somewhat reactive with respect to the superconducting material under expected manufacturing conditions. In the preferred embodiments made using a PIT process, it must also be readily formable and must allow good oxygen access to the filaments under the expected manufacturing conditions.
  • Preferred jacketing materials include silver and other noble metals, and their alloys, particularly ODS silver and silver-gold alloys.
  • the matrix and jacketing layer may be formed simultaneously from the same noble metal, and a post-processing step added to increase the resistivity of the jacketing layer by, for example, ion bombardment.
  • the intermediate is thermomechanically processed at conditions sufficient to produce at least one of the effects of texturing, crack healing and, if a precursor to the desired superconducting oxide remains, phase transformation in the filament material under conditions which support the electrical separation of the domains.
  • the intermediate is thermomechanically processed at conditions sufficient to produce at least one of the effects of passivating any predecessor material and forming an insulating material in the decoupling layers and texturing, crack healing and, if a precursor to the desired superconducting oxide remains, phase transformation in the filament material.
  • the thermomechanical processing step comprises the steps of first heat treating the composite at conditions sufficient to passivate the predecessor and form an insulating material from at least part of the predecessor material but not to activate the filament materials, and, thereafter activating the filaments by thermomechanical treatment at conditions sufficient to produce at least one of the effects of texturing, crack healing and, if a precursor to the desired superconducting oxide remains, phase transformation in the filament material.
  • condition which activate the filament materials are meant conditions which enable substantial chemical and/or thermodynamic phase transformations in these materials (but not the matrix) .
  • texturing as that term is used herein, is meant inducing crystallographic alignment and intergrain bonding of the grains of a desired superconducting oxide or its precursors.
  • the preliminary heat treatment step is continued until the metal predecessor layers are essentially passivated by thorough oxidation of the interface between the metal predecessor layers and the adjoining matrix before any substantial thermomechanical activation of the precursors takes place. Passivation may take place either by formation of an oxide scale on these surfaces or by essentially complete oxidation of the entire metal predecessor layer.
  • preliminary heat treatment in an oxidizing atmosphere at a temperature of less than about 700 degrees C, and preferably less than about 550 C, for up to 100 hours has been found to adequately oxidize the predecessor layers under conditions where the precursors are kinetically limited. Thermomechanical activation of the intermediate may then be performed in accordance with conventional PIT processing methods.
  • passivation may not be completed until thermomechanical activation of the precursors has begun, but the predecessor materials and passivation conditions may be selected so that the oxygen flux associated with the passivation reactions does not interfere with the desired phase evolution of the precursors, for example, by annealing at very high oxygen pressures, preferably greater than about 10 atmospheres.
  • FIGs 4, 5 and 6 are schematic diagrams of three alternative processing sequences for the preliminary heat treatment and thermomechanical filament activation steps in accordance with these preferred embodiments of the invention.
  • a separate preliminary heat treatment step 402 may be done at a fixed temperature prior to the initiation of thermomechanical activation 404.
  • the preliminary heat treatment may take place during the ramp-up 502 to thermomechanical activation conditions, 504, with one or more plateaus, as illustrated by FIG 5, or continuously, but at a very slow ramp rate, preferably less than 10 C/min as illustrated by 602 in FIG 6.
  • the duration of the preliminary heat treatment step will determine whether the predecessor is fully passivated prior to activation of the filament material.
  • thermomechanical activation may be continued as required to obtain optimal performance in the superconducting composite.
  • the thermomechanical processing step comprises the step of texturing, crack healing and, if a precursor to the desired superconducting oxide remains, phase transformation in the filament material at conditions selected so that any activation of the insulating material does not significantly impair its insulating properties or interfere with the desired phase transformations of the filament materials.
  • selection of an appropriate insulating material is essential.
  • the insulating material must be flowable enough to handle the substantial deformations typical of superconducting composite manufacturing processes.
  • insulating materials possess either a work hardening rate or a strain rate sensitivity which provide sufficient flowability in combination with the other required characteristics.
  • Powders or bulk forms of boron nitride, tungsten carbide, titanium carbide, silicon carbide, alumina, silicon nitride, boron carbide, zirconium oxide, titanium nitride, yttrium oxide, or magnesium oxide may be used.
  • FIGs 7 and 8 illustrate alternate forms of multifilamentary composite articles manufactured in accordance with the invention.
  • the matrix portion 704 of round composite wire 700 is separated into a plurality of separate domains 718, 720, 722, 724, 726 by multiple filament decoupling layers 706, 708, 710, 712.
  • the filament decoupling layers have a closed geometry in that each forms a closed loop in cross-section which completely encloses the cross- sections of one or more filaments 714, 716.
  • the material for the filament decoupling layers is selected to be a material which is oxygen permeable under the activation conditions for the filaments.
  • zirconium or zirconium oxide filament decoupling layers may be used in combination with BSCCO 2223 filaments.
  • each domain might contain a single filament.
  • a jacketing layer 702 of conductive material surrounds the matrix.
  • the jacketing layer may be a composite material including both conductive and non- conductive portions.
  • a highly aspected tape 800 is shown in which filament decoupling layer 806 forms a central spine and additional filament decoupling layers form radiating legs 808, 810, 812, 814, 816, 818, 820, 822, 824, 826, 828, 830 which separate the matrix 804 into domains 838, 840, 842, 844, 846, 848, 850, 852, 854, 856, 858, 860 each containing one or more filaments, for example filament 832, of superconducting oxide material
  • a tape in this form may be manufactured in accordance with the invention by first, forming a hollow tube having an outer wall 804 of a suitable matrix material and an inner wall comprising a filament decoupling layer 806; second, forming an intermediate by inserting additional filament decoupling layers 808, 810, 812, 814, 816, 818, 820, 822, 824, 826, 828, 830 at spaced intervals between the inner
  • filaments may be included in each domain.
  • deforming the intermediate to flatten the tube, twist the filaments and texture the material comprised therein; and finally, thermomechanically processing the intermediate as described above.
  • microcracking of the filament decoupling layers during the deformation step may provide improved oxygen access to the filaments during thermomechanical processing.
  • a round wire is shown in FIG 7 and a rectangular tape is shown in FIG 8, but articles in a variety of forms may be manufactured in accordance with the invention.
  • Round filaments are shown in Fig 7 and 8 but any aspect ratio and any cross-section, such as square, hexagonal, octagonal, or trapezoidal, may equally be used.
  • fine filaments should be used.
  • fine filaments are meant filaments with a maximum transverse cross-sectional dimension less than 750 , and preferably less than 150 microns.
  • High aspect ratio filaments with an aspect ratio of about 10:1, and a thickness less than about 75 microns, may be used.
  • precursor powders and composite subunits may be formed using one of the standard PIT techniques.
  • nitrate powders comprising the precursors of BSCCO 2223 may be packed in standard silver billets, and extrusion and wire-drawing may be used to form hexagonal monofilamentary rods.
  • a plurality of these rods may be assembled in a close-packed manner, and filament decoupling layers of oxide forming materials preferably selected from the group consisting of zirconium, niobium, molybdenum and their alloys may be inserted among the rods in a predetermined geometry to define a plurality of separate domains.
  • the assembly steps may be repeated as often as required to obtain an intermediate composite with the desired number and arrangement of domains such as, for example, those shown in FIGs 1, 6 or 7. If a jacketing layer is desired, the entire assembly may be inserted into a conductive tube. Composites with up to 10,000 domains, but only a small number of fine filaments per domain, are preferred.
  • a succession of deformation steps including but not limited to drawing, twisting and rolling, may be used to reduce the diameter of the intermediate to a value in the range of from 0.01 inch to 0.12 inch (0.025 to 0.3 cm), and preferably 0.02 inch to 0.06 inch (0.05 to 0.153 cm), and to obtain a desired twist pitch, preferably at least on the order of the width of the intermediate.
  • the intermediate may be wire- drawn to a diameter in the range of 0.15 inch to 0.02 inch (0.038 to 0.05 cm) twisted to about 20 twists per inch (a twist pitch of 1.25 mm) and then rolled in one or more reduction passes to a maximum transverse cross-sectional dimension in the range of 0.05 inch to 0.005 inch (0.127 to 0.013 cm) . If multiple deformations are performed, intermediate anneals will preferably be performed in between.
  • the intermediate may be subjected to a preliminary heat treatment step in an oxidizing atmosphere at a temperature of less than about 700 degrees C, and preferably less than about 550 degrees C, for up to 100 hours in order to oxidize the decoupling layers under conditions where the BSCCO precursors are kinetically limited.
  • the intermediate may then be heat treated at 750 870 C for 1-100 hours at 0.001 to 1 atmosphere oxygen to promote texturing and achieve proper oxygenation of the BSCCO precursors.
  • a final heat treatment may be performed in a 7.5% oxygen atmosphere at 828 to 832 c for 20 to 80 hours, 805 to 815 C for 1 to 240 hours and 787 to 795 C for 10 to 50 hours to form and sinter the desired 2223 material in the filament cores and to promote crack healing.
  • Precursor powders were prepared from the solid state reaction of freeze-dried precursors of the appropriate metal nitrates having the nominal composition of 1.8:0.3:1.9:2.0:3.1 (Bi:Pb:Sr:Ca:Cu) .
  • Bi 2 0 3 , CaC0 3/ SrC0 3 , Pb 3 0 4 and CuO powders could equally be used.
  • a multistep treatment typically 3-4 steps
  • calcination 800°C+_10°C, for a total of 15 h
  • intermediate grinding was performed in order to remove residual carbon, homogenize the material and generate a BSCCO 2212 oxide superconductor phase.
  • the powders were packed into silver sheaths having an inner diameter of 0.850 inch (2.16 cm) and a length of 8 inch (20.32 cm) and an outer diameter of 1.25 inch (3.18 cm) to form a billet.
  • the billets were extruded to a diameter of 1/2 inch (1.27 cm).
  • the billet diameter was narrowed with multiple die steps, with a final step drawn through a 0.70 inch (1.78 cm) hexagonally shaped die into a silver/precursor hexagonal wires.
  • the billet was drawn to 0.18 inch (0.46 cm) via successive 20% pass reductions and then annealed at 450 C in air for 4 hours, drawn to 0.072 inch (0.183 cm) via successive 20% and 10% pass reductions, annealed at 450 C in air for 2 hours, and finally drawn to .0.04 inch ( 1.02 cm) and annealed at 450 C in air for 4 hours to form a multifilamentary round intermediate.
  • Two nickel-containing and two control portions (0X1026N with filament decoupling layers and 0X1026 without) were then taken from the intermediate.
  • Example 1 was ramped up to 400 C at 10 C/minute, to 700 C at 1 C/minute and then to 830 C at 0.1 C/minute in a 7.5% oxygen atmosphere and immediately given a final heat treatment in a 7.5% oxygen atmosphere at 830 C for 40 hours, 811 C for 40 hours and 787 C for 30 hours to form and sinter the desired 2223 material in the filament cores and produce a thin nickel oxide layer.
  • Example 2 was ramped up to 500 C at 10 C/minute and immediately given a short high oxidation treatment at 500 C for 4 hours in a 100% oxygen atmosphere, then equilibrated at 500 C for 4 hours in a 7.5% oxygen atmosphere, followed by a ramp up to 830 C at l C/minute and the same final heat treatment used for Example 1, to form and sinter the desired 2223 material in the filament cores and produce a moderate nickel oxide layer.
  • Example 3 was ramped up to 500 C at 10 C/minute and immediately given a long high oxidation treatment at 500 C for 4 hours in a 100% oxygen atmosphere and then equilibrated at 500 C for 16 hours in a 7.5% oxygen atmosphere, followed by followed by a ramp up to 830 C at 1 C/minute and the same final heat treatment used for Example 1 to form and sinter the desired 2223 material in the filament cores and produce a thick nickel oxide layer.
  • Example 4 was ramped up to 450 C at 10 C/minute and then to 500 C at 2 C/minute in 100% oxygen atmosphere and given a high pressure oxidation treatment at 500 C for 20 hours at 100 atm (1500 psi) , allowed to equilibrate to room temperature and pressure and then ramped up to 350 C at 10 C/minute and then to 400 C at 2 C/minute in 100% oxygen atmosphere and given an equilibration cycle at 400 C for 40 hours at 7.5%, followed by the same final heat treatment used for Example 1 to form and sinter the desired 2223 material in the filament cores and produce a very thick nickel oxide layer.
  • the critical current of Examples 1-3 were measured at 77K, using a 1 V/cm criteria and a 1 cm voltage tap length.
  • the critical currents of the experimental conductors were determined using a four-point probe technique.
  • Engineering critical current densities were calculated for all samples as the measured critical current separated by the cross-sectional area of the wire. Averages reported are the averages of two samples. N indicates the samples which included filament decoupling layers. Thickness and width measurements are in inches.
  • a multifilamentary composite intermediate article may be made using filament decoupling layers in the form of insulating materials and the intermediate then processed to form a superconducting composite.
  • Boron nitride or tungsten carbide powders may be packed into six silver sheaths, each having an inner diameter of 0.850 inch (2.16 cm) and a length of 8 inch (20.32 cm) and an outer diameter of 1.25 inch (3.18 cm) to form six billets.
  • powders of titanium carbide, silicon carbide, alumina, silicon nitride, boron carbide, zirconium oxide, titanium nitride, yttrium oxide, or magnesium oxide may be used.
  • Each billet may be drawn by a series of 10% reduction passes to a diameter of 0.200 inch (0.51 cm) and then rolled by a series of 10% reduction passes to a tape with a thickness of 0.005 inch (0.013 cm).
  • Each of these tapes may be used as a filament decoupling layer.
  • Hexagonal monofilamentary wires of silver/BSCCO 2223 precursor may be prepared as described in Examples 1-8.
  • Each of the tapes may be bent into the shape of a gutter and three wires placed in it. Then the six bent tapes may be bundled together, with their open sides facing outwards, around a central silver rod with a diameter of 0.070 inch (0.178 cm), to form six separate domains containing three wires each, and the entire assembly inserted into a tubular silver jacketing layer having an inner diameter of 0.387 inch (0.982 cm) and an outer diameter of 0.42 inch (1.067 cm) to form a billet.
  • the billet may be drawn to 0.18 inch (0.457 cm) via successive 20% pass reductions and then annealed at 400 C in air for 1 hour, drawn to 0.072 inch ( cm) via successive 20% and 10% pass reductions, annealed at 400 C in air for 1 hour, and finally drawn to .0.04 inch ( 0.102 cm) and annealed at 400 C in air for 1 hour to form a multifilamentary round intermediate.
  • Example 9 may be thermomechanically processed by ramping up to 830 C at 1 C/minute in a 7.5% oxygen atmosphere and immediately giving a final heat treatment in a 7.5% oxygen atmosphere at 830 C for 40 hours, 811 C for 40 hours and 787 C for 30 hours to form and sinter the desired 2223 material in the filament cores.
  • a multifilamentary YBCO composite intermediate article may be made using filament decoupling layers in the form of alumina scale formers and the intermediate then processed to form a superconducting composite.
  • the precursor may be prepared as described in U.S. Patent No. 5,034,373 or US Patent Application S.N. 07/881,675 filed 5/12/92, which are incorporated herein by reference.
  • An alloy of Y-Ba-Cu-Ag or Y(Ca)-Ba-Cu-Ag, with, preferably the appropriate stoichiometry of metallic constituents to form a 1-2-4 type oxide superconductor may be packed as a powder into a silver sheath having an inner diameter of 0.05 inch (1.25 cm), a length of 8 inch (20.32 cm), and an outer diameter of 0.06 inch (1.57 cm) .
  • Silver powder typically comprising 10-50 weight % of the total powder, should be included with the alloy.
  • the packed billet may be welded shut under a protective atmosphere and then reduced in diameter by warm hydrostatic extrusion at 325C to form monofilamentary wires.
  • Eighteen of the wires may be bundled together around a central aluminum/copper alloy rod [10% aluminum, 90% copper] with a diameter of 0.070 inch (0.18 cm), which had previously been annealed for 2 hours at 600 C in a reducing atmosphere, and six sheets of the same aluminum/copper alloy, each made from a double thickness of 0.005 inch (0.127 cm) foil (99.7% pure) may be inserted among the wires to form six domains containing three wires each.
  • the bundle may be drawn to 0.18 inch (0.46 cm) via successive 20% pass reductions and then annealed at 450 C in air for 4 hours, drawn to 0.072 inch (0.18 cm) via successive 20% and 10% pass reductions, annealed at 450 C in air for 2 hours, and finally drawn to .0.04 inch ( 0.10 cm) and annealed at 450 C in air for 4 hours to form a multifilamentary round intermediate.
  • the intermediates may be rebundled with additional aluminum/copper alloy sheets and rods, and the reduction process repeated as often as desired to obtain an intermediate of the desired dimensions with the desired number of domains.
  • the resulting intermediate may be thermomechanically processed by oxidizing in pure oxygen at 500 C for 300-400 hours, and then deformed at room temperature by 2 to 6 iterations of, for example, pressing at 13,000 to 35,000 pounds load force or rolling by successive 10 to 20% pass reductions alternating with anneals for 0.1 to 10 hours at 650-800 C to obtain a multifilamentary superconducting composite.
  • a multifilamentary BSCCO 2212 composite intermediate article may be made using closed zirconium filament decoupling layers and the intermediate then processed to form a superconducting composite.
  • the precursor may be prepared as described in Phase Alignment in Ag-Clad 2212 Bi-Sr-Ca-Cu-O Wires, R. D . Ray II & E. E. Hellstrom, Applied Physics Letters, 57, 2948-2950 (1990) , which is incorporated herein by reference.
  • Precursor powders may be prepared from reagent grade Bi 2 0 3 , CaC0 3 SrC0 3 , and CuO powders with a nominal Bi:Sr:Ca:Cu mole ration of 2:2:1:2.
  • a multistep treatment typically 3-4 steps
  • calcination 800°C - 825°C, for a total of 48 h
  • isostatic pressing 280 MPa
  • intermediate grinding may be performed in order to remove residual carbon, homogenize the material and generate a BSCCO 2212 oxide superconductor phase.
  • the powders may be packed into zirconium-coated silver sheaths having, for example, an inner diameter of 0.850 inch (2.16 cm) and a length of 8 inch (20.32 cm) and an outer diameter (silver layers) of 1.25 inch (3.18 cm) and a sputtered 2 micron thick outer coating of zirconium to form billets and drawn to 0.055 inch (0.138 cm) via one or more pass reductions, with one or more intermediate anneals at 400 C in air for 1 hour..
  • the billets may be bundled together around a central silver rod with a diameter of 0.070 inch (0.18 cm) and the entire assembly inserted into a tubular silver jacketing layer having an inner diameter of 0.170 inch (0.43 cm) and an outer diameter of 0.210 inch (0.53 cm) to form a composite billet.
  • the billet may be drawn to a 0.055 inch (0.138 cm) diameter round via one or more pass reductions with one or more intermediate anneals at 400 C in air for 1 hour, twisted to a 2.54 inch (1 cm) twist pitch, annealed as before, and finally rolled to a final cross-section of about 0.12 inch (0.3 cm) by 0.004 inch (0.01 cm) to form a multifilamentary intermediate article.
  • the intermediate may be heated at 5C/min to 920 C, held for 15 minutes, cooled at 10 to 240 C to 840 C, annealed at 840 C for 70 hours, all in air and finally air cooled at room temperature to obtain a multifilamentary superconducting composite tape.

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Abstract

L'invention concerne un article composite supraconducteur (100) à plusieurs filaments. Cet article comprend de multiples domaines (106, 108, 110, 112, 114, 116) sensiblement électriquement découplés, comprenant chacun un ou plusieurs filaments fins (130, 132, 134), de préférence torsadés d'un matériau d'oxyde supraconducteur requis. Dans un mode de réalisation préféré, l'article (100) comprend une matrice (104) qui comprend, sensiblement, un métal noble, une couche de gainage conductrice (102) entourant la matrice (104), plusieurs couches discrètes (118, 120, 122, 124, 126, 128, 136) de découplage des filaments. Chacune de ces couches comprend un matériau isolant, et est disposée à l'intérieur de la matrice (104) pour séparer cette dernière (104) en plusieurs domaines (106, 108, 110, 112, 114, 116) sensiblement électriquement découplés: plusieurs filaments (130, 132, 134), comprenant chacun un oxyde supraconducteur requis, sont disposés à l'intérieur de la matrice (104) et sensiblement enveloppés par cette dernière, et ainsi chimiquement isolés des couches de découplage (118, 120, 122, 124, 126, 128, 136). Chacun des domaines électriquement découplés (106, 108, 110, 112, 114, 116) contient au moins un filament (130, 132, 134). On obtient ainsi des articles (100) à plusieurs filaments qui présentent de fortes caractéristiques de puissance de courant continu et de puissance de courant alternatif, nettement supérieures à celles des matériaux actuellement disponibles. L'invention concerne également un procédé et un produit intermédiaire pour réaliser cet article (100).
PCT/US1996/007061 1995-05-19 1996-05-17 Composite supraconducteur a plusieurs filaments et procede de fabrication WO1996036485A1 (fr)

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EP96914661A EP0828606A4 (fr) 1995-05-19 1996-05-17 Composite supraconducteur a plusieurs filaments et procede de fabrication
AU57956/96A AU709214B2 (en) 1995-05-19 1996-05-17 A multifilamentary superconducting composite and method of manufacture
JP53505796A JP3444893B2 (ja) 1995-05-19 1996-05-17 マルチフィラメント状超伝導性複合材料および製法
NZ308348A NZ308348A (en) 1995-05-19 1996-05-17 Multifilamentary superconducting composite, with multiple electrically decoupled domains

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US08/444,564 1995-05-19

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EP0828606A1 (fr) 1998-03-18
US6038462A (en) 2000-03-14
CA2220930A1 (fr) 1996-11-21
US6393690B1 (en) 2002-05-28
EP0828606A4 (fr) 1999-09-08
JP3444893B2 (ja) 2003-09-08
AU709214B2 (en) 1999-08-26
JPH11505365A (ja) 1999-05-18
CN1190366A (zh) 1998-08-12
AU5795696A (en) 1996-11-29
NZ308348A (en) 1998-09-24
CN1096935C (zh) 2002-12-25

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